@inproceedings{f46cfa5acc9f43518f48c268b0532873,
title = "Research on setting method of neutral plane offset of shell element in prseus panel structure modeling",
abstract = "The PRSEUS panel structure meets the design requirements of high lift drag ratio and low fuel consumption of wing body fusion aircraft. In the finite element analysis software ABAQUS, the modeling method of setting different offsets on skin, flange and tear strap is adopted to compare the influence of different shell element offsets on the first-order buckling eigenvalues, and the accurate shell element neutral plane offsets are obtained by comparing the test results, It provides a reference for accurate modeling of similar panel structures.",
keywords = "Neutral offset, PRSEUS, Shell element",
author = "Yongjie Zhang and Yingying Wu",
note = "Publisher Copyright: {\textcopyright} 2021 IEEE.; 12th International Conference on Mechanical and Aerospace Engineering, ICMAE 2021 ; Conference date: 16-07-2021 Through 19-07-2021",
year = "2021",
month = jul,
day = "16",
doi = "10.1109/ICMAE52228.2021.9522501",
language = "英语",
series = "2021 12th International Conference on Mechanical and Aerospace Engineering, ICMAE 2021",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "91--95",
booktitle = "2021 12th International Conference on Mechanical and Aerospace Engineering, ICMAE 2021",
}